Sukhoi Su-17UM3

Sukhoi Su-17

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VrstaSovjetska napadalna letala
Prvi let2. avgust 1966
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Fotogalerija Sukhoi Su-17UM3.

V Sukhoi Su-17 (Nato poročevalsko ime: Fitter) je sovjetsko napadalno letalo, razvito iz lovca-bombnika Suhoi Su-7. Imela je dolgo kariero v sovjetski, kasneje ruski, službi in je bila na splošno izvožena v komunistične in bližnje vzhodne zračne sile, pod imeni Su-20 in Su-22.

Vir: Sukhoi Su-17UM3 na Wikipediji

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V Sukhoi Su-17UM3 is a two-seat, advanced operational trainer variant of the venerable Soviet Su-17 variable-sweep wing fighter-bomber (NATO designation “Fitter”). It was developed from the earlier Su-17UM, incorporating the improved avionics and systems of the single-seat Su-17M3 ground-attack aircraft.


Design and Role

Trainer Configuration:

  • Primary role is to provide advanced training and conversion for pilots transitioning to the high-performance Su-17/22 family of attack jets.
  • It features a tandem two-seat cockpit, with the instructor occupying the rear seat.
  • The aircraft utilizes a raised, deeper dorsal spine (similar to the single-seat Su-17M3) to accommodate additional avionics and fuel tankage, compensating for the weight and space taken up by the second cockpit.

Variable-Sweep Wings:

  • Like all Su-17 variants, the Su-17UM3 uses the signature variable-sweep outer wing panels, allowing for excellent low-speed handling (takeoff/landing) and high-speed performance (supersonic flight) in a single airframe.
  • The sweep angle can be configured between approximately 30° and 63°.

Operational Capability:

  • Although primarily a trainer, the Su-17UM3 retains significant combat capability, sharing the weapon hardpoints and weapon delivery systems of the single-seat variants.
  • It is typically powered by the Lyulka AL-21F-3 afterburning turbojet engine (unlike some export trainers, the Su-22UM3, which used the Tumansky R-29 engine).

General Specifications (Approximate, based on Su-17M3/UM3 data)

Funkcija Specifikacija
Vrsta Advanced Two-Seat Trainer / Fighter-Bomber
Posadke 2 (Pilot and Instructor/Trainee)
Motor Lyulka AL-21F-3 Afterburning Turbojet
Max Speed Approx. Mach 1.7 (High Altitude) / Mach 1.1 (Sea Level)
Main Armament Two 30 mm Nudelman-Rikhter **NR-30** cannons
Payload Capacity Up to 4,000 kg (8,800 lbs) of ordnance (bombs, rockets, missiles, gun pods)
Wingspan (Unswept) Approx. 13.68 m (44 ft 11 in)
Dolžina Approx. 19.02 m (62 ft 5 in)

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